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팽창기 사이클 수소 로켓엔진의 시스템 해석
System Analysis of Expander Cycle Hydrogen Rocket Engine 원문보기

한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.24 no.5, 2020년, pp.21 - 33  

하동휘 (Department of Aerospace Engineering, Inha University) ,  노태성 (Department of Aerospace Engineering, Inha University) ,  이형진 (Department of Aerospace Engineering, Inha University) ,  유필훈 (LIG Nex1)

초록
AI-Helper 아이콘AI-Helper

본 연구에서는 액체 수소를 연료로 사용하는 팽창기 사이클 로켓 엔진의 시스템 해석을 위한 프로그램을 개발하였다. 수소의 물성치는 온도에 따른 이성질체의 비율을 고려하였다. 팽창기 사이클 엔진의 개방형과 폐쇄형 형식에 따른 해석 절차를 수립하고 부품별 해석 방법을 제시하였다. 본 해석 프로그램의 검증을 위해 팽창기 사이클 엔진인 Vinci와 SE-21D를 대상으로 엔진 작동점의 성능 및 국외에서 수행된 해석 결과와 비교하였다. 해석 결과, 입력 정보가 부정확한 일부를 제외한 추진제의 질유량, 비추력, 동력과 같은 시스템의 주요 성능 인자는 1~2% 내외의 오차로 높은 정확도를 나타내었다.

Abstract AI-Helper 아이콘AI-Helper

In this study, the program for system analysis of an expander cycle rocket engine using liquid hydrogen as a fuel was developed. The properties of hydrogen were considered by the ratio of isomers with temperature. The analysis procedure was established with the open and closed types of the expander ...

주제어

참고문헌 (36)

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